View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40024U 14033Q 23087.42282408 .00009653 00000-0 89272-3 0 9995
2 40024 98.0205 40.6345 0010622 178.1506 181.9754 14.94733465476342
| Epoch (UTC): | 28 March 2023 10:08:52 |
| Eccentricity: | 0.0010622 |
| inclination: | 98.0205° |
| perigee height: | 576 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 40.6345° |
| argument of perigee: | 178.1506° |
| revolutions per day: | 14.94733465 |
| mean anomaly at epoch: | 181.9754° |
| orbit number at epoch: | 47634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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